JP2785519B2 - Internal combustion engine cooling system - Google Patents
Internal combustion engine cooling systemInfo
- Publication number
- JP2785519B2 JP2785519B2 JP16697591A JP16697591A JP2785519B2 JP 2785519 B2 JP2785519 B2 JP 2785519B2 JP 16697591 A JP16697591 A JP 16697591A JP 16697591 A JP16697591 A JP 16697591A JP 2785519 B2 JP2785519 B2 JP 2785519B2
- Authority
- JP
- Japan
- Prior art keywords
- refrigerant
- annular
- cylinder liner
- annular groove
- internal combustion
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Landscapes
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Description
【0001】[0001]
【産業上の利用分野】本発明は内燃機関の冷却装置に係
り、特にシリンダライナ外周に環状溝を設けて冷媒を流
し、内燃機関の冷却を行なう冷却装置に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a cooling device for an internal combustion engine, and more particularly to a cooling device for cooling an internal combustion engine by providing an annular groove around an outer periphery of a cylinder liner to flow a refrigerant.
【0002】[0002]
【従来の技術】数個のシリンダが配置されたシリンダブ
ロックと、そのシリンダブロック上面に位置し、下面に
へこみを有するシリンダヘッドとは、内燃機関の燃焼室
を形造っている。また、シリンダブロックのボア部内周
面にシリンダライナ外周面が嵌装される。従って、機関
作動により燃焼室で発生した高温の熱はシリンダブロッ
クやシリンダヘッドを通じてシリンダライナ等へ伝達さ
れる。2. Description of the Related Art A cylinder block in which several cylinders are arranged, and a cylinder head located on the upper surface of the cylinder block and having a depression on the lower surface form a combustion chamber of an internal combustion engine. Further, an outer peripheral surface of the cylinder liner is fitted to an inner peripheral surface of the bore of the cylinder block. Therefore, high-temperature heat generated in the combustion chamber by the operation of the engine is transmitted to the cylinder liner and the like through the cylinder block and the cylinder head.
【0003】そこで、シリンダライナの壁面を冷却する
と共に、冷媒の沸騰を防止するために、シリンダブロッ
クのボア部内周面とシリンダライナ外周面との間に冷媒
通路を形成し、その冷媒通路に冷媒を流すようにした所
謂グルーブクーリングによる内燃機関の冷却装置が従来
より知られている(例えば、実開昭63−168242
号公報)。In order to cool the wall surface of the cylinder liner and prevent the refrigerant from boiling, a refrigerant passage is formed between the inner peripheral surface of the bore of the cylinder block and the outer peripheral surface of the cylinder liner. 2. Description of the Related Art A cooling device for an internal combustion engine by so-called groove cooling in which air flows is conventionally known (for example, Japanese Utility Model Application Laid-Open No. 63-168242).
No.).
【0004】図4は上記の従来の内燃機関の冷却装置の
一例の構造図を示し、同図(A)は平面図、同図(B)
は同図(A)のB−B線に沿う縦断面図を示す。図4
(A),(B)において、シリンダブロック1に嵌装さ
れるシリンダライナ2の外周面には、例えば31 〜34
で示す如く断面矩形状の環状溝がシリンダライナ2の軸
方向に4個形成されている。この環状溝31 〜34 はシ
リンダライナ2をシリンダブロック1のボア部内に嵌装
したとき、ボア部の内周面4との間で環状の冷媒通路を
形成する。FIG. 4 is a structural view of an example of the above-mentioned conventional cooling device for an internal combustion engine, wherein FIG. 4A is a plan view and FIG.
Shows a vertical cross-sectional view along the line BB in FIG. FIG.
(A), (B), the the outer circumferential surface of the cylinder liner 2 is fitted to the cylinder block 1 is for example 3 1 to 3 4
As shown in the figure, four annular grooves having a rectangular cross section are formed in the axial direction of the cylinder liner 2. The annular groove 3 1 to 3 4 when fitted to the cylinder liner 2 into the bore portion of the cylinder block 1, to form a refrigerant passage of an annular between the inner circumferential surface 4 of the bore portion.
【0005】また、シリンダライナ2とシリンダブロッ
ク1との互いに対向する位置で、かつ、シリンダライナ
2の軸方向(縦方向)に、上記の複数の環状溝31 〜3
4 の間を連通する縦溝5と6が形成されている。また、
シリンダブロック1の最もシリンダヘッド側の位置に
は、縦溝5に連通した冷媒導入口7が形成され、また縦
溝6に連通した冷媒導出口8が形成されている。The plurality of annular grooves 3 1 to 3 are positioned at positions where the cylinder liner 2 and the cylinder block 1 face each other and in the axial direction (longitudinal direction) of the cylinder liner 2.
Vertical grooves 5 and 6 communicating between the four are formed. Also,
At the position of the cylinder block 1 closest to the cylinder head, a refrigerant inlet 7 communicating with the vertical groove 5 is formed, and a refrigerant outlet 8 communicating with the vertical groove 6 is formed.
【0006】また、燃焼室で発生し、シリンダライナ2
へ伝達される熱は、燃焼室に近づくほど(図4(B)の
断面図の上部ほど)シリンダライナ壁面の温度を高くさ
せるため、シリンダライナ2の壁面温度が均一となるよ
うに冷却するために、環状溝の断面積が燃焼室に近い環
状溝ほど、すなわち34 →33 →32 →31 の順で小と
されている。[0006] Further, it is generated in the combustion chamber, and the cylinder liner 2
In order to increase the temperature of the cylinder liner wall surface as it approaches the combustion chamber (upward in the cross-sectional view of FIG. 4B), the heat transferred to the combustion chamber is cooled so that the wall surface temperature of the cylinder liner 2 becomes uniform. to, and is about the annular groove close to the cross-sectional area of the annular groove combustion chamber, that is, 3 4 → 3 3 → 3 2 → 3 1 small in the order.
【0007】上記の従来の冷却装置によれば、冷媒導入
口7から導入された冷媒は、縦溝5を図4(B)中、上
から下方向へ流れつつ環状溝31 〜33 に分配され縦溝
5の底部に達した冷媒は最下部の環状溝34 に流れ込
む。複数個の環状溝31 〜34 を図4(B)中、X方向
へ夫々通過する冷媒は、その際にシリンダライナ2の外
周壁面の熱を奪いつつ、かつ、上部の環状溝ほど断面積
が小であるので大なる速度で流れて縦溝6に到り、ここ
で集合された後、冷媒導出口8より外部のラジエータを
通して循環ポンプ(いずれも図示せず)へ導出され、そ
の後再び冷媒導入口7に到る。According to the conventional cooling device of the above, the refrigerant introduced from the refrigerant inlet port 7, the longitudinal grooves 5 in FIG. 4 (B), the annular groove 3 1 to 3 3 while flowing downward from the top the refrigerant that has reached the bottom of the distributed longitudinal grooves 5 flows into the annular groove 3 4 the bottom. In the figure a plurality of annular grooves 3 1 ~3 4 4 (B) , the refrigerant respectively pass through the X-direction, while absorbing heat of the outer peripheral wall surface of the cylinder liner 2 in this case, and, as the upper part of the annular groove cross Since the area is small, it flows at a high speed to reach the vertical groove 6, where it is gathered, then led out of the refrigerant outlet 8 through an external radiator to a circulation pump (neither shown), and then again. The refrigerant inlet 7 is reached.
【0008】このように、上記の従来装置によれば、燃
焼室で発生し、シリンダライナ2へ伝達される熱を、シ
リンダライナ2の壁面の入熱分布に応じた速度(温度が
高い所ほど速い)で冷媒を循環させることにより、シリ
ンダライナ2の壁面を略均一に冷却することができる。As described above, according to the above-described conventional apparatus, the heat generated in the combustion chamber and transmitted to the cylinder liner 2 is converted into a velocity (a higher temperature where the temperature is higher) in accordance with the heat input distribution on the wall surface of the cylinder liner 2. By circulating the refrigerant at (fast), the wall surface of the cylinder liner 2 can be cooled substantially uniformly.
【0009】[0009]
【発明が解決しようとする課題】しかるに、上記の従来
装置では、図5に示す如く、冷媒導入口7に流入した冷
媒は縦溝5を介して殆ど流路を曲げられることなく最上
部の環状溝31 に流入するのに対して、最上部から2番
目以降の環状溝32 ,33 に対してはa,bで示す如く
流路が直角に曲げられて流入する。しかし、冷媒は高速
で縦溝5を流れるために慣性によって直角に流路が変化
するのは困難である。このため、環状溝3 2 ,33 等の
最上部から2番目以降の環状溝では図5にc及びdに夫
々示す如く各環状溝32 ,33 の冷媒入口部の上流位置
で淀みが発生する。この淀みは、最上部より2番目の環
状溝32 においてcで示す如く最も大きく、下部の環状
溝3 3 ,34 ほど緩和される傾向にある。これは、縦溝
5での冷媒の流速は、流量の低下に伴って下部ほど低く
なるため、慣性効果がaで示す上部位置で最も大きく、
以下下部に行くほど減少するためである。SUMMARY OF THE INVENTION However, the above-mentioned conventional
In the apparatus, as shown in FIG.
The medium is the uppermost part without being able to bend the flow path through the vertical groove 5.
Annular groove 31While the second from the top
Annular groove 3 after eyesTwo, 3ThreeAs shown by a and b
The flow path is bent at a right angle and flows in. But the refrigerant is fast
Flow changes at right angles due to inertia to flow in vertical groove 5
It is difficult to do. For this reason, the annular groove 3 Two, 3ThreeEtc.
In the second and subsequent annular grooves from the top, the c and d in FIG.
Each annular groove 3 as shownTwo, 3ThreeUpstream of the refrigerant inlet
Causes stagnation. This stagnation is the second ring from the top
Groove 3TwoThe largest, as shown by c, the lower ring
Groove 3 Three, 3FourTend to be moderated. This is a flute
5, the lower the flow rate of the refrigerant, the lower the lower the flow rate
Therefore, the inertia effect is greatest at the upper position indicated by a,
This is because it decreases as going to the lower part.
【0010】このような淀みが入熱量の多いシリンダラ
イナ2の上部で発生すると、冷媒が沸騰し、その結果発
生した冷媒中の空気が循環ポンプ内に滞留して循環ポン
プの出力流量を低下させるため、ラジエータで冷却不調
となりオーバーヒートの原因となるおそれがある。When such stagnation occurs in the upper portion of the cylinder liner 2 having a large amount of heat input, the refrigerant boils, and the resulting air in the refrigerant stays in the circulation pump to reduce the output flow rate of the circulation pump. As a result, the radiator may malfunction due to cooling, which may cause overheating.
【0011】本発明は上記の点に鑑みなされたもので、
各循環溝の冷媒入口の上流位置に案内部材を設けること
により、上記の課題を解決した内燃機関の冷却装置を提
供することを目的とする。[0011] The present invention has been made in view of the above points,
An object of the present invention is to provide a cooling device for an internal combustion engine that solves the above-mentioned problems by providing a guide member at a position upstream of a refrigerant inlet of each circulation groove.
【0012】[0012]
【課題を解決するための手段】上記課題を解決するた
め、本発明ではシリンダブロックと該シリンダブロック
に嵌装されるシリンダライナとの間に該シリンダライナ
の周方向に沿って形成され、かつ、該シリンダライナの
軸方向に複数形成された環状通路と、前記シリンダライ
ナの軸方向に延在し、かつ、互いに異なる位置で前記複
数の環状通路間を夫々連通するように設けられた第1及
び第2の連通路と、前記第1の連通路に冷媒を供給する
ための冷媒導入口と、前記複数の環状通路及び前記第2
の連通路を通った冷媒を排出するための冷媒導出口とを
有する内燃機関の冷却装置において、前記冷媒導入口か
ら導入されて前記第1の連通路を通る冷媒が、前記複数
の環状通路のうち前記冷媒導入口の延在方向上になく、
かつ、前記第1の連通路の延在方向と略直交する方向に
分流されて導入される環状通路の、冷媒入口上流部に、
冷媒を環状通路方向へ案内する案内部材を設けたもので
ある。In order to solve the above problems SUMMARY OF THE INVENTION, in the present invention is formed along a circumferential direction of the cylinder liner between the cylinder liner which is fitted to the cylinder block and the cylinder block, and, A plurality of annular passages formed in the axial direction of the cylinder liner, and first and second annular passages extending in the axial direction of the cylinder liner and provided so as to communicate between the plurality of annular passages at positions different from each other. A second communication path, a refrigerant inlet for supplying a refrigerant to the first communication path, the plurality of annular paths, and the second communication path;
In the cooling device for an internal combustion engine having a refrigerant outlet for discharging the refrigerant that has passed through the communication passage, the refrigerant that is introduced from the refrigerant introduction port and passes through the first communication passage is formed of the plurality of annular passages. Of which, not in the direction of extension of the refrigerant inlet,
And in the upstream portion of the refrigerant inlet of the annular passage which is diverted and introduced in a direction substantially perpendicular to the extending direction of the first communication passage ,
A guide member for guiding the refrigerant in the direction of the annular passage is provided.
【0013】[0013]
【作用】冷媒導入口から導入されて第1の連通路を通る
冷媒が、複数の環状通路のうち前記冷媒導入口の延在方
向上になく、かつ、前記第1の連通路の延在方向と略直
交する方向に分流されて導入される環状通路の冷媒入口
上流部に淀みが発生する。そこで、本発明ではこの淀み
が発生する環状通路の冷媒入口上流部に、冷媒を前記案
内部材により積極的に導入するようにしたため、淀みは
上記案内部材を介して導入された冷媒により解消され
る。The refrigerant introduced from the refrigerant inlet and passing through the first communication passage is not in the extending direction of the refrigerant introduction port among the plurality of annular passages, and the extending direction of the first communication passage. Stagnation occurs in the upstream portion of the refrigerant inlet of the annular passage which is diverted and introduced in a direction substantially perpendicular to the direction. Therefore, in the present invention, since the refrigerant is positively introduced by the guide member into the upstream of the refrigerant inlet of the annular passage where the stagnation occurs, the stagnation is eliminated by the refrigerant introduced through the guide member. .
【0014】[0014]
【実施例】図1は本発明になる内燃機関の冷却装置の一
実施例の要部構成図で、同図(A)は半截平面図、同図
(B)は断面図を示す。同図(A),(B)において、
シリンダブロック11に嵌装されるシリンダライナ12
の外周面には環状溝131 ,132 ,133 ,…が形成
されているため、シリンダライナ12をシリンダブロッ
ク11のボア部内に嵌装することにより、環状溝1
31 ,132 ,133 ,…とボア部内周面とにより環状
通路が形成される。FIG. 1 is a schematic view of a main part of an embodiment of a cooling device for an internal combustion engine according to the present invention. FIG. 1 (A) is a half plan view and FIG. 1 (B) is a sectional view. In the figures (A) and (B),
Cylinder liner 12 fitted to cylinder block 11
Annular grooves 13 1 on the outer peripheral surface of, 13 2, 13 3, ... it is formed by fitted the cylinder liner 12 into the bore portion of the cylinder block 11, an annular groove 1
3 1, 13 2, 13 3, annular passage is formed by the ... and the bore inner peripheral surface.
【0015】また、シリンダライナ12とシリンダブロ
ック11に、環状溝131 〜133 等をシリンダライナ
12の軸方向に連通する縦溝14が前記第1の連通路と
して形成され、また図示は省略したが、図1(A)の平
面図上、縦溝14と180°異なる位置にも環状溝13
1 〜133 等をシリンダライナ12の軸方向に連通する
縦溝が前記第2の連通路として形成されている。シリン
ダブロック11のシリンダヘッド側の部分には縦溝14
と連通する冷媒導入口15がシリンダライナ12の軸方
向と直交する方向に形成されているため、冷媒導入口1
5の延在方向上に環状溝131 133 のうち最もシリン
ダヘッド側の環状溝131 が位置する。一方、最上部か
ら2番目以降の下部の環状溝32 ,33等は冷媒導入口
15の延在方向上になく、かつ、前記縦溝14の延在方
向(シリンダライナ12の軸方向)と略直交する方向に
冷媒が分流されて導入される環状通路である。本実施例
はかかる構造の冷却装置において、図1(A),(B)
に示す如く、最上部から2番目以降の下部の環状溝
32 ,33等の冷媒入口部の縦溝14部分に、案内部材
161 ,162を設けた点に特徴がある。Further, the cylinder liner 12 and the cylinder block 11, is formed an annular groove 131-134 3 such as the first communication passage longitudinal groove 14 which communicates with the axial direction of the cylinder liner 12, also not illustrated However, on the plan view of FIG.
Longitudinal grooves communicating 1-13 3 etc. in the axial direction of the cylinder liner 12 is formed as the second communication path. A vertical groove 14 is provided in the cylinder block 11 on the cylinder head side.
Is formed in a direction perpendicular to the axial direction of the cylinder liner 12, the refrigerant introduction port 15 communicating with the
Annular groove 13 of the most cylinder head side of the annular groove 13 1 13 3 is located at the 5 in the extending direction on. On the other hand, the annular groove 3 2 at the bottom of the second and subsequent from the top, 3 3, etc. is not in the extending direction of the refrigerant inlet port 15, and (the axial direction of the cylinder liner 12) extending direction of the longitudinal grooves 14 This is an annular passage into which the refrigerant is diverted and introduced in a direction substantially orthogonal to. This embodiment relates to a cooling device having such a structure, as shown in FIGS.
As shown in, the longitudinal groove 14 portion of the refrigerant inlet portion, such as the lower portion of the annular groove 3 2, 3 3 of the second and subsequent from the top, it is characterized in that provided guide members 16 1, 16 2.
【0016】ここで、案内部材161 ,162 は断面が
矩形状で、かつ、平面が頂点を環状溝132 ,133 方
向に向けた三角形状とされている。また、案内部材16
1 は図1(B)に示す如く、幅Lの環状溝132 の上半
分の幅1/2L内に位置するように配設され、環状溝1
32 の冷媒入口上流部に冷媒を案内する構成とされてい
る。案内部材162 も上記と同様に環状溝133 の冷媒
入口上流部に冷媒を案内する構成とされている。[0016] Here, in the guide member 16 1, 16 2 in cross-section a rectangular shape, and are plane vertex an annular groove 13 2, 13 3 triangular shape toward the direction. Also, the guide member 16
1 as shown in FIG. 1 (B), is arranged so as to be positioned in the annular groove 13 within the width 1 / 2L of the upper half of the second width L, an annular groove 1
Refrigerant inlet upstream of the 3 2 is configured to guide the refrigerant into. Guiding member 16 2 is also configured to guide the refrigerant to the refrigerant inlet upstream portion of the same annular groove 13 3.
【0017】次に本実施例の作用について説明する。冷
媒導入口15に導入された冷媒は図1(B)中、Iで示
す如く右方向へ進み、殆ど流路を曲げられることなく直
進してIIで示す如く最もシリンダ側の環状溝131 に流
入する一方、冷媒の一部は縦溝14内をIII で示す如く
下方向へ進み案内部材161 により一部が環状溝13 2
の冷媒入口上流部に案内され、残りが環状溝132 の冷
媒入口下流部や案内部材162 へ導かれる。以下、上記
と同様にして冷媒は環状溝133 の冷媒入口上流部にIV
で示す如く案内部材162 により案内される一方、縦溝
14内を下方向へ導入される。なお、図1(A)中、実
線の矢印は環状溝131 〜133 の冷媒の流れの方向を
示す。Next, the operation of this embodiment will be described. cold
The refrigerant introduced into the medium introduction port 15 is indicated by I in FIG.
Proceed to the right, and straight
As shown by II, the annular groove 13 closest to the cylinder side1Flow
While a part of the refrigerant enters the vertical groove 14 as indicated by III.
Guide member 16 that moves downward1Partly due to the annular groove 13 Two
Is guided to the upstream of the refrigerant inlet, and the remainingTwoCold
Medium inlet downstream part and guide member 16TwoLed to. Below,
In the same manner as inThreeIV upstream of the refrigerant inlet
Guide member 16 as shown byTwoFlutes while guided by
14 is introduced downward. Note that, in FIG.
The arrow of the line is the annular groove 131~ 13ThreeThe direction of the refrigerant flow
Show.
【0018】前記したように、従来は特に環状溝132
に導入される冷媒は、流速が速いために流路がシリンダ
ライナ12の軸方向と直交する方向へ曲がりきらないた
め、環状溝132 の冷媒入口上流位置に淀みが発生す
る。これに対し、本実施例では冷媒が案内部材161 に
より環状溝132 の冷媒入口上流位置に積極的に案内さ
れると共に、環状溝132 の冷媒入口下流位置には案内
部材161 と縦溝14の壁面との間を通過した冷媒の一
部が流入するため、前記した淀みは発生しない。従っ
て、淀みによる冷媒の沸騰も発生せず、オーバーヒート
を防止することができる。As described above, conventionally, the annular groove 13 2
Refrigerant introduced into, because the flow path for the flow velocity is high is not completely bent in a direction perpendicular to the axial direction of the cylinder liner 12, stagnation occurs in refrigerant inlet upstream position of the annular groove 13 2. In contrast, the refrigerant is positively guided to the refrigerant inlet upstream position of the annular groove 13 2 by the guide members 16 1 in this embodiment, the guide member 16 1 to the refrigerant inlet downstream position of the annular groove 13 2 Vertical Since a part of the refrigerant that has passed between the wall of the groove 14 flows in, the above-mentioned stagnation does not occur. Accordingly, the refrigerant does not boil due to stagnation, and overheating can be prevented.
【0019】なお、各環状溝131 〜133 に導入され
た冷媒は、各環状溝131 〜133 を流れつつシリンダ
ライナ12の外周壁面の熱を奪い、その後縦溝14と対
向する位置にある縦溝に流れ込み、ここで集合されて冷
媒導出口より導出される。[0019] Incidentally, the refrigerant introduced into the annular grooves 131-134 3 deprives the heat of the outer peripheral wall surface of the cylinder liner 12 while flowing through each of the annular grooves 131-134 3, then the vertical grooves 14 and a position facing Flows into the vertical groove, and is collected here and discharged from the refrigerant outlet.
【0020】次に本発明の他の実施例について説明す
る。図2は本発明になる内燃機関の冷却装置の他の実施
例の要部断面図を示す。同図中、図1と同一構成部分に
は同一符号を付し、その説明を省略する。図2におい
て、211 及び212 は夫々案内部材で、環状溝1
32 ,133の冷媒入口上流部に冷媒を案内するための
部材で、断面及び平面が夫々三角形状であり、前記案内
部材161 及び162 と同様に縦溝14内の位置に配設
されている。Next, another embodiment of the present invention will be described. FIG. 2 is a sectional view showing a main part of another embodiment of the cooling device for an internal combustion engine according to the present invention. In the figure, the same components as those of FIG. 1 are denoted by the same reference numerals, and description thereof will be omitted. In FIG. 2, reference numerals 21 1 and 21 2 denote guide members, respectively.
3 2, 13 3 of a member for guiding the refrigerant to the refrigerant inlet upstream section, a cross-sectional and plane respectively triangular, disposed at the position of the guide member 16 1 and 16 2 similarly to the longitudinal grooves 14 Have been.
【0021】これにより、本実施例によれば、図1に示
した実施例に比し、案内部材211 ,212 はテーパが
設けられているためより管路抵抗少なく環状溝132 ,
13 3 の冷媒入口上流位置に冷媒を案内することができ
る。従って、本実施例は前記実施例と同様に淀みの発生
を防止できる。Thus, according to the present embodiment, as shown in FIG.
The guide member 21 is1, 21TwoHas a taper
The annular groove 13 has less pipeline resistance because of being provided.Two,
13 ThreeRefrigerant can be guided to the refrigerant inlet upstream position
You. Therefore, in this embodiment, the occurrence of stagnation occurs as in the previous embodiment.
Can be prevented.
【0022】なお、本発明は上記の各実施例に限定され
るものではなく、例えば図3の断面図に示す如く、環状
溝131 〜133 をシリンダライナ12の軸方向に連通
する縦溝31が、シリンダブロック11上のシリンダヘ
ッド32側に延在されて冷媒導入口33に連通された構
造の冷却装置では、最もシリンダヘッド32側に位置す
る環状溝131 よりも更にシリンダヘッド32側に位置
する冷媒導入口33より冷媒が導入されるため、環状溝
131 は冷媒導入口33の延在方向上にはなく、他の環
状溝132,133 と同様に冷媒が縦溝31の延在方向
と略直交する方向に分流されて導入される冷媒通路を構
成している。[0022] Incidentally, the longitudinal grooves present invention which communicates is not limited to the embodiments described above, for example, as shown in the sectional view of FIG. 3, the annular groove 131-134 3 in the axial direction of the cylinder liner 12 31, extending in the cylinder head 32 side of the cylinder block 11 by a cooling device communicated with the structure to the refrigerant inlet 33, further cylinder head 32 side of the annular groove 13 1 located most cylinder head 32 side since the refrigerant is introduced from the refrigerant inlet 33 located in an annular groove 13 1 is not on the extending direction of the refrigerant inlet 33, the other annular groove 13 2, 13 3 and likewise refrigerant longitudinal grooves 31 And a refrigerant passage which is branched and introduced in a direction substantially perpendicular to the extending direction of the refrigerant.
【0023】従って、かかる構造の冷却装置では、図3
に示す如く最もシリンダヘッド32側に位置する環状溝
131 の冷媒導入部上流位置付近の縦溝31にも、他の
環状溝132 及び133 の各冷媒導入部上流位置付近の
縦溝31に設けられた案内部材342 ,343 と同様
に、冷媒を案内するための案内部材341 が設けられ
る。Therefore, in the cooling device having such a structure, FIG.
Longitudinal grooves 31 in the vicinity of the most longitudinal groove 31 in the vicinity of the refrigerant inlet portion upstream position of the annular groove 13 1 is located in the cylinder head 32 side, the refrigerant inlet portion upstream position of the other annular groove 13 2 and 13 3 as shown in similar to the guide member 34 2, 34 3 provided on, are provided guide members 34 1 for guiding the refrigerant.
【0024】これにより、冷媒導入口33より導入され
た冷媒は、縦溝31内を図3中、下方向へ流れながら各
環状溝131 〜133 に分配される。このとき、案内部
材341 〜343 で各環状溝131 〜133 の冷媒入口
上流位置に冷媒が供給されるため、淀みの発生を防止す
ることができる。[0024] Accordingly, the refrigerant introduced from the refrigerant inlet port 33, in Figure 3 the longitudinal grooves 31, is distributed to each of the annular grooves 131-134 3 while flowing downward. In this case, since the refrigerant is supplied by the guide members 34 1 to 34 3 to the refrigerant inlet upstream position of the annular grooves 131-134 3, it is possible to prevent the occurrence of stagnation.
【0025】また、本発明は冷媒導入口をシリンダヘッ
ドに最も遠い位置に設けた冷却装置にも適用することが
できる。この場合は、冷媒導入口から導入された冷媒は
縦溝をシリンダヘッド方向に流れつつ、複数の環状溝に
分配されるため、冷媒導入口の延長上にない環状溝のう
ち最もシリンダヘッドに遠い位置にある環状溝に、冷媒
が流路を縦溝の軸方向に対して直角に曲げられ、かつ、
大きな流速で流れ込むため最も淀みが発生し易い。その
ため、このような冷却装置においても各環状溝の冷媒入
口上流部に冷媒を案内するための案内部材を縦溝に設け
ることにより、上記の淀みの発生を防止することができ
る。The present invention can also be applied to a cooling device provided with a refrigerant inlet at a position farthest from the cylinder head. In this case, the refrigerant introduced from the refrigerant introduction port is distributed to the plurality of annular grooves while flowing in the vertical groove in the direction of the cylinder head, and is the furthest to the cylinder head among the annular grooves that are not on the extension of the refrigerant introduction port. The coolant is bent at right angles to the axial direction of the vertical groove in the annular groove at the position, and,
Stagnation is most likely to occur because of the flow at a large flow velocity. Therefore, even in such a cooling device, the generation of the above-mentioned stagnation can be prevented by providing the guide member for guiding the refrigerant to the upstream portion of the refrigerant inlet of each annular groove in the vertical groove.
【0026】[0026]
【発明の効果】上述の如く、本発明によれば、冷媒の流
路中に淀みが発生し易い環状通路の冷媒導入部に積極的
に冷媒を導入するようにしたため、淀みの発生を防止す
ることができ、よって淀みに起因する沸騰を防止でき、
オーバーヒートを未然に防止することができる等の特長
を有するものである。As described above, according to the present invention, the refrigerant is positively introduced into the refrigerant introduction portion of the annular passage in which stagnation is likely to occur in the refrigerant flow path, thereby preventing stagnation. Can prevent boiling caused by stagnation,
It has features such as being able to prevent overheating beforehand.
【図1】本発明になる内燃機関の冷却装置の一実施例の
要部構成図である。FIG. 1 is a main part configuration diagram of an embodiment of a cooling device for an internal combustion engine according to the present invention.
【図2】本発明になる内燃機関の冷却装置の他の実施例
の要部断面図である。FIG. 2 is a sectional view of a main part of another embodiment of a cooling device for an internal combustion engine according to the present invention.
【図3】本発明になる内燃機関の冷却装置の更に他の実
施例の要部断面図である。FIG. 3 is a cross-sectional view of a main part of still another embodiment of the cooling device for an internal combustion engine according to the present invention.
【図4】従来の内燃機関の冷却装置の一例の構成図であ
る。FIG. 4 is a configuration diagram of an example of a conventional cooling device for an internal combustion engine.
【図5】発明が解決しようとする課題の説明図である。FIG. 5 is an explanatory diagram of a problem to be solved by the invention.
11 シリンダブロック 12 シリンダライナ 131 〜133 環状溝 14 縦溝(第1の連通路) 15,33 冷媒導入口 161 ,162 ,211 ,212 ,341 〜343 案
内部材DESCRIPTION OF SYMBOLS 11 Cylinder block 12 Cylinder liner 13 1 to 13 3 Annular groove 14 Vertical groove ( first communication path) 15, 33 Refrigerant inlet 16 1 , 16 2 , 21 1 , 21 2 , 34 1 to 34 3 Guide member
───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平1−167448(JP,A) 実開 昭63−168242(JP,U) (58)調査した分野(Int.Cl.6,DB名) F02F 1/14 F02F 1/16 F01P 3/02──────────────────────────────────────────────────続 き Continuation of the front page (56) References JP-A-1-167448 (JP, A) JP-A-63-168242 (JP, U) (58) Fields investigated (Int. Cl. 6 , DB name) F02F 1/14 F02F 1/16 F01P 3/02
Claims (1)
に嵌装されるシリンダライナとの間に該シリンダライナ
の周方向に沿って形成され、かつ、該シリンダライナの
軸方向に複数形成された環状通路と、前記シリンダライ
ナの軸方向に延在し、かつ、互いに異なる位置で前記複
数の環状通路間を夫々連通するように設けられた第1及
び第2の連通路と、前記第1の連通路に冷媒を供給する
ための冷媒導入口と、前記複数の環状通路及び前記第2
の連通路を通った冷媒を排出するための冷媒導出口とを
有する内燃機関の冷却装置において、 前記冷媒導入口から導入されて前記第1の連通路を通る
冷媒が、前記複数の環状通路のうち前記冷媒導入口の延
在方向上になく、かつ、前記第1の連通路の延在方向と
略直交する方向に分流されて導入される環状通路の、冷
媒入口上流部に、冷媒を環状通路方向へ案内する案内部
材を設けたことを特徴とする内燃機関の冷却装置。An annular passage formed between a cylinder block and a cylinder liner fitted to the cylinder block along a circumferential direction of the cylinder liner, and a plurality of annular passages formed in an axial direction of the cylinder liner. A first and a second communication passage extending in the axial direction of the cylinder liner and provided so as to communicate between the plurality of annular passages at different positions from each other; A refrigerant inlet for supplying a refrigerant, the plurality of annular passages and the second
And a refrigerant outlet for discharging the refrigerant that has passed through the communication passage of the internal combustion engine, wherein the refrigerant introduced from the refrigerant introduction port and passing through the first communication passage is connected to the plurality of annular passages. Of the annular passage, which is not in the direction in which the refrigerant introduction port extends and is introduced by being diverted in a direction substantially perpendicular to the direction in which the first communication passage extends , the refrigerant is annularly formed in the upstream portion of the refrigerant inlet. A cooling device for an internal combustion engine, comprising a guide member for guiding in the direction of a passage .
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16697591A JP2785519B2 (en) | 1991-07-08 | 1991-07-08 | Internal combustion engine cooling system |
| US07/906,499 US5207189A (en) | 1991-07-08 | 1992-06-30 | Cooling system for an internal combustion engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP16697591A JP2785519B2 (en) | 1991-07-08 | 1991-07-08 | Internal combustion engine cooling system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH0518317A JPH0518317A (en) | 1993-01-26 |
| JP2785519B2 true JP2785519B2 (en) | 1998-08-13 |
Family
ID=15841084
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP16697591A Expired - Fee Related JP2785519B2 (en) | 1991-07-08 | 1991-07-08 | Internal combustion engine cooling system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2785519B2 (en) |
-
1991
- 1991-07-08 JP JP16697591A patent/JP2785519B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0518317A (en) | 1993-01-26 |
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